Modeling A ============== Characteristics of modeling ----------------------------------- .. image:: images/Object_14.svg :width: 627 :height: 211 .. _RefImage_Object_14.svg: Characteristics of the mesh ---------------------------- Number of knots: 43 Number of meshes and type: 20 TRIA3 Tested values --------------- +------------------------------------------------------------------------------------+------------------+-----------+-------------+---------+----------------+ | |**Identification**|**Moments**|**Reference**|**Aster**|**% difference**| + .. image:: images/Object_15.svg + + + + + + | :width: 627 | | | | | | + :height: 211 + + + + + + | | | | | | | + + + + + + + | | | | | | | +------------------------------------------------------------------------------------+------------------+-----------+-------------+---------+----------------+ |5 |ETA_PILOTAGE |5 |1.0 |1.11133 |11.11 | +------------------------------------------------------------------------------------+------------------+-----------+-------------+---------+----------------+ |25 |ETA_PILOTAGE |15 |1.0 |1.142 |11.42 | +------------------------------------------------------------------------------------+------------------+-----------+-------------+---------+----------------+ notes --------- In this analysis, an imposed displacement type resolution technique ('DDL_IMPO') is used to find the solution. This method provides for each imposed displacement value, a load multiplier coefficient ('ETA_PILOTAGE'). The value of the load imposed in 'AFFE_CHAR_MECA' is equal to the limit pressure, therefore the reference value of the parameter 'ETA_PILOTAGE' is equal to 1. The calculations were stopped when the value of parameter ETA_PILOTAGE stabilized. The reference being taken in relation to the beam solution with 50 elements, we observe an improvement in the DKT TRIA3 results when the mesh is refined.